Turbine engine with fuel nozzle

A turbine engine comprising:

• a compressor section, combustor section, and turbine section in serial flow arrangement, with the combustor section including a fuel nozzle assembly comprising:
• a fuel nozzle including a fuel passage defining a longitudinal axis, the fuel nozzle terminating at a nozzle tip;
• a swirler defining a swirler passage about the fuel nozzle, having a forward wall spaced from an aft wall, and having a center wall positioned between the forward wall and the aft wall;
• a set of vanes provided within the swirler;
• a lip extending downstream from the center wall relative to a flow direction through the swirler, and the lip terminating at an aft end;
• and
• a purge opening extending through the forward wall and exhausting to the swirler passage;
• wherein the nozzle tip is positioned aft of the aft end of the lip relative to the longitudinal axis.